Alternative Anode Material for Solid Oxide Fuel Cells

ABSTRACT

Anode materials comprising various compositions of strontium iron cobalt molybdenum oxide (SFCM) for low- or intermediate-temperature solid oxide fuel cell (SOFCs) are provided. These materials offer high conductivity achievable at intermediate and low temperatures and can be used to prepare the anode layer of a SOFC. A method of making a low- or intermediate temperature SOFC having an anode layer including SFCM is also provided.

BACKGROUND OF THE INVENTION Field of The Invention

This invention relates to solid oxide fuel cell (SOFC) anode materialsthat comprise various compositions of a strontium iron cobalt molybdenumoxide (SFCM). These materials offer high conductivity achievable atintermediate and low temperatures and can be used to prepare the anodelayer of a SOFC. A method of making a low- or intermediate-temperatureSOFC having an anode layer including SFCM is also provided.

Background

SOFCs are electrochemical energy conversion devices that can directlyconvert hydrogen or hydrocarbons into electrical power with highefficiencies. Conventionally, SOFCs operate a high temperatures (˜800°C.), which limits the choice of materials for SOFC components.Furthermore, high temperature operation leads to rapid degradation ofSOFC components. Lowering the operating temperature of SOFCs canovercome such issues; however, electrode resistance increases due tosluggish reaction kinetics, affecting the overall fuel cell efficiency.

Typically, the anode forms the principal structural component of SOFCsand therefore, it is critical that the anode material should be highlyefficient. For traditional SOFC anode materials, porous Ni-YSZ or Ni-GDCcomposites are often fabricated to achieve both high ionic conductivityand high electronic conductivity. However, even though nickel is highlyelectronically conductive and catalytically active, there are problemswith it, such as volume change during thermal and reduction-oxidationcycling, carbon deposition when using hydrocarbon fuels, and low sulfurtolerance. Considering these issues, electronically conductive ceramicsoffer a promising alternative to nickel-based anodes. And, ceramic oxidebased anodes are also a potential replacement for conventional Ni-GDCanodes considering their tolerance toward coking and sulfur poisoning.But, the electronic conductivity and catalytic activity for hydrogenoxidation for ceramic anodes are much lower than with Ni-GDC anodes.Application of ceramic anodes for low temperature operating SOFCs isstill being researched. And, ceramic anodes suffer from severalfabrication challenges such as thermal mismatch, chemical stability andincompatibilities with other components (e.g., electrolyte).Furthermore, the conductivity of electronically conductive ceramics ismuch lower than nickel, which is deleterious to the performance ofSOFCs.

Others have developed all-ceramic anode materials with acceptableconductivity for SOFCs. Such anode materials include niobium dopedstrontium titanate (SNT), which can have good electronic conductivity(˜6.5 S-cm⁻¹) after reduction at ˜930° C. and shows goodreduction-oxidation stability. SNT and alternative conductive ceramicsfor SOFC anodes require conductivity activation by high temperaturesintering of the material in a reducing environment or in situ reductionat high temperatures. However, neither of these options is feasible forintermediate or low-temperature SOFCs.

Thus, there is a need for an improved low temperature anode material foruse within solid oxide fuel cells. There is a need for newelectronically conductive ceramic materials that meet both theconductivity and stability requirements of the anode and are compatiblewith intermediate- and low-temperature operation.

SUMMARY OF THE INVENTION

Some embodiments include a solid-oxide fuel cell having a cathode layer;an electrolyte layer; and an anode layer. The anode layer including astrontium iron cobalt molybdenum oxide material.

In one embodiment, the disclosure provides a solid-oxide fuel cellcomprising: a cathode layer; an electrolyte layer; and an anode layer,the anode layer comprising a strontium iron cobalt molybdenum (SFCM)oxide material.

In another embodiment, the disclosure provides a solid oxide fuel cell,wherein the anode layer is configured to allow electron percolationthrough the strontium iron cobalt molybdenum oxide material.

In another embodiment, the disclosure provides a solid oxide fuel cell,wherein the SFCM oxide material has the formula:

SrM¹ _(x)M² _(((1−x)2))Mo_(((1−x)/2))O_(3±δ)

wherein M¹ and M² are different transition metals and are not Mo, x isabout 0.1-0.5; and δ is about 0-1.5. In one embodiment, M¹ is Fe and M²is Co.

In another embodiment, the disclosure provides a solid oxide fuel cell,wherein the SFCM oxide material has the formula:

SrM¹ _(x)M² _(y)Mo_(z)O₃

wherein M¹ and M² are different transition metals and are not Mo, x isabout 0.1-0.5; y is about 1−x; and z is about 1−x. In one embodiment, M¹is Fe and M² is Co.

In another embodiment, the disclosure provides a solid oxide fuel cell,wherein x is about 0.1-0.4. In another embodiment, x is about 0.1-0.3.In another embodiment, x is about 0.1-0.25.

In another embodiment, the disclosure provides a solid oxide fuel cell,wherein the cathode layer comprises a composite comprising:

(a) a material selected from the group consisting of lanthanum strontiumcobalt iron oxide (LSCF), barium strontium cobalt iron oxide (BSCF),samarium strontium cobalt iron oxide (SSCF), samarium strontium cobaltoxide (SSC), and lanthanum strontium manganate (LSM); and

(b) a material selected from the group consisting of yttria stabilizedzirconia (YSZ), scandia stabilized zirconia (SSZ), gadolinia doped ceria(GDC), samaria doped ceria (SDC), samaria-neodymium doped ceria (SNDC),erbia stabilized bismuth oxide (ESB), dysprosium tungsten stabilizedbismuth oxide (DWSB), yttria stabilized bismuth oxide (YSB), andstrontium and magnesium doped lanthanum gallate (LSGM).

In another embodiment, the disclosure provides a solid oxide fuel cell,wherein the cathode layer comprises a composite comprising SSC and GDC.

In another embodiment, the disclosure provides a solid oxide fuel cell,wherein the electrolyte layer comprises a material selected from thegroup consisting of YSZ, SSZ, GDC, SDC, SNDC, ESB, DWSB, YSB, and LSGM.

In another embodiment, the disclosure provides a solid oxide fuel cell,wherein the electrolyte layer comprises GDC.

In another embodiment, the disclosure provides a solid oxide fuel cell,wherein the anode layer has a conductivity of between 10 S/cm and 100S/cm when measured at a temperature between 350° C. and 850° C.

In another embodiment, the disclosure provides a solid oxide fuel cell,wherein the anode layer has a conductivity of between 10 S/cm and 100S/cm when measured at a temperature between 350° C. and 650° C.

In another embodiment, the disclosure provides a solid oxide fuel cell,wherein the anode layer has a conductivity of between 10 S/cm and 40S/cm when measured at a temperature between 350° C. and 850° C.

In another embodiment, the disclosure provides a solid oxide fuel cell,wherein the anode layer has a conductivity of between 10 S/cm and 40S/cm when measured at a temperature between 350° C. and 650° C.

In another embodiment, the disclosure provides a solid oxide fuel cell,wherein the anode layer has a conductivity of between 30 S/cm and 40S/cm when measured at a temperature between 350° C. and 850° C.

In another embodiment, the disclosure provides a solid oxide fuel cell,wherein the anode layer has a conductivity of between 30 S/cm and 40S/cm when measured at a temperature between 350° C. and 650° C.

In another embodiment, the disclosure provides a solid oxide fuel cell,further comprising a cathode functional layer disposed between theelectrolyte layer and the cathode layer. In another embodiment, thecathode functional layer comprises LSCF, BSCF, SSCF, SSC, YSZ, SSZ, GDC,SDC, SNDC, ESB, DWSB, YSB, LSGM, or combinations thereof. In anotherembodiment, the cathode functional layer comprises GDC.

In another embodiment, the disclosure provides a solid oxide fuel cell,wherein the anode layer comprises only oxide materials.

In another embodiment, the disclosure provides a solid oxide fuel cell,wherein the anode layer is porous.

In another embodiment, the disclosure provides a solid oxide fuel cell,wherein the anode layer further comprises GDC.

In another embodiment, the disclosure provides a solid oxide fuel cell,wherein the anode layer further comprises cobalt doped GDC.

In another embodiment, the disclosure provides a solid oxide fuel cell,wherein the anode layer is infiltrated with Ni or Ni-GDC.

In another embodiment, the disclosure provides a solid oxide fuel cell,wherein the anode layer is infiltrated with a multivalent transitionmetal, e.g., Fe.

In another embodiment, the disclosure provides a solid oxide fuel cell,wherein the anode layer comprises SrFe_(0.1)CO_(0.45)Mo_(0.45)O₃,SrFe_(0.2)Co_(0.4)Mo_(0.4)O₃, SrFe_(0.34)Co_(0.33)Mo_(0.33)O₃, orSrFe_(0.5)Co_(0.25)Mo_(0.25)O₃.

In another embodiment, the disclosure provides an oxide compositioncomprising:

SrM¹ _(x)M² _(((1−x)/2))Mo_(((1−x)/2))O_(3±δ)

wherein M¹ and M² are different transition metals and are not Mo, x isabout 0.1-0.5; and δ is about 0-1.5. In one embodiment, M¹ is Fe and M²is Co.

In another embodiment, the disclosure provides an oxide compositioncomprising:

SrM¹ _(x)M² _(y)Mo_(z)O₃

wherein M¹ and M² are different transition metals and are not Mo, x isabout 0.1-0.5; y is about 1−x; and z is about 1−x. In one embodiment, M¹is Fe and M² is Co.

In another embodiment, the disclosure provides an oxide composition,wherein x is about 0.1-0.4. In another embodiment, x is about 0.1-0.3.In another embodiment, x is about 0.1-0.25.

In another embodiment, the disclosure provides an oxide compositioncomprising SrFe_(0.1)Co_(0.45)Mo_(0.45)O₃, SrFe_(0.2)Co_(0.4)Mo_(0.4)O₃,SrFe_(0.34)Co_(0.33)Mo_(0.33)O₃, or SrFe_(0.5)Co_(0.25)Mo_(0.25)O₃.

In another embodiment, the disclosure provides an oxide composition,which comprises SrFe_(0.2)Co_(0.4)Mo_(0.4)O₃.

In another embodiment, the disclosure provides an oxide composition,which comprises SrFe_(0.1)Co_(0.45)Mo_(0.45)O₃.

In another embodiment, the disclosure provides a method of making thesolid oxide fuel cell comprising: (a) fabricating the cathode layer, theelectrolyte layer, and the anode layer; and (b) forming a complete cellwith the fabricated layers in (a); wherein the temperature of anysubsequent fabrication steps, and the operating temperature of the solidoxide fuel cell, is between 350° C. and 850° C.

In another embodiment, the disclosure provides a method of making asolid oxide fuel cell, wherein the temperature of any subsequentfabrication steps, and the operating temperature of the solid oxide fuelcell, is between 350° C. and 650° C.

In another embodiment, the disclosure provides a method of making asolid oxide fuel cell further comprising at least one additional layerfabricated with the cathode layer, the electrode layer, and the anodelayer to form the complete cell; and wherein the temperature of anysubsequent fabrication steps, and the operating temperature of the solidoxide fuel cell, is between 350° C. and 850° C.

In another embodiment, the disclosure provides a method of making asolid oxide fuel cell, wherein the temperature of any subsequentfabrication steps, and the operating temperature of the solid oxide fuelcell, is between 350° C. and 650° C.

In another embodiment, the disclosure provides a method of making asolid oxide fuel cell, wherein the at least one additional layer is acathode functional layer.

In another embodiment, the disclosure provides a method of making asolid oxide fuel cell, wherein the anode layer comprisesSrFe_(0.1)Co_(0.45)Mo_(0.45)O₃, SrFe_(0.2)Co_(0.4)Mo_(0.4)O₃,SrFe_(0.34)Co_(0.33)Mo_(0.33)O₃, or SrFe_(0.5)Co_(0.25)Mo_(0.25)O₃.

In another embodiment, the disclosure provides a method of making asolid oxide fuel cell, wherein the anode layer comprisesSrFe_(0.2)Co_(0.4)Mo_(0.4)O₃.

In another embodiment, the disclosure provides a method of making asolid oxide fuel cell, wherein the anode layer comprisesSrFe_(0.1)Co_(0.45)Mo_(0.45)O₃.

BRIEF DESCRIPTION OF THE DRAWINGS

The accompanying drawings, which are incorporated herein and form a partof the specification, illustrate one or more embodiments of the presentinvention and, together with the description, further serve to explainthe principles of the invention and to enable a person skilled in thepertinent art to make and use the invention. The following drawings aregiven by way of illustration only, and thus are not intended to limitthe scope of the present invention.

FIG. 1A shows a fuel cell comprising a cathode, an electrolyte layer,and an anode according to one embodiment.

FIG. 1B shows a fuel cell comprising a cathode, a cathode functionallayer, an electrolyte layer, and an anode layer according to oneembodiment.

FIG. 2 shows a schematic of a solid oxide fuel cell (SOFC) comprising a15-20 μm Sr_(0.5)Sm_(0.5)CoO₃-gadolinia doped ceria (SSC-GDC) cathodelayer, a 5 μm 2 mol % cobalt doped GDC cathode functional layer, a 20-30μm GDC electrolyte layer, and a glycine-nitrate process (GNP) strontiumiron cobalt molybdenum oxide-gadonlina doped ceria (SFCM-GDC) compositeanode layer infiltrated with Ni-GDC (˜10 wt % loading) according to oneembodiment.

FIG. 3 shows a schematic of a SOFC comprising a 15-20 μm SSC-GDC layer,a 20-30 μm GDC layer, and a GNP SFCM-GDC composite anode layerinfiltrated with Ni-GDC (˜10 wt % loading) according to one embodiment.

FIG. 4 shows a graph comparing the conductivities of various anodematerials (SrCo_(0.5)Mo_(0.5)O₃ (SFCM#1), SrFe_(0.1)Co_(0.45)Mo_(0.45)O₃(SFCM#2), SrFe_(0.2)Co_(0.4)Mo_(0.4)O₃ (SFCM#3),SrFe_(0.34)Co_(0.33)Mo_(0.33)O₃ (SFCM#4), andSrFe_(0.5)Co_(0.25)Mo_(0.25)O₃ (SFCM#5)) reduced in 10% H₂/90% N₂ forabout 24 hours.

FIG. 5 is a plot of open circuit voltage (left scale) and power density(right scale) for a complete SOFC constructed withSrFe_(0.2)Co_(0.4)Mo_(0.4)O₃ (SFCM#3) composite anode, according to anembodiment of the invention, at various temperatures.

FIG. 6 shows Nyquist plots of a complete SOFC constructed with SFCM#3composite anode, according to an embodiment of the invention, at varioustemperatures.

FIG. 7 shows a cross sectional scanning electron microscope (SEM) imageof a complete fuel cell comprising a SSC-GDC cathode layer, a Co-GDCcathode functional layer, a GDC electrolyte layer, and a SFCM#3 anodelayer according to one embodiment.

FIG. 8 shows a cross sectional SEM image of an SFCM#3 anode according toone embodiment.

FIG. 9 shows a cross sectional SEM image of an SFCM#3 anode according toone embodiment.

FIG. 10 shows a cross sectional SEM image of a SFCM#3 anode infiltratedwith Ni-GDC anode according to one embodiment.

DETAILED DESCRIPTION

This specification discloses one or more embodiments that incorporatethe features of this invention. The disclosed embodiment(s) merelyexemplify the invention. The scope of the invention is not limited tothe disclosed embodiment(s). Multiple inventions may be described. Theinvention is defined by the claims appended hereto.

The embodiment(s) described, and references in the specification to “oneembodiment,” “an embodiment,” “an example embodiment,” etc., indicatethat the embodiment(s) described may include a particular feature,structure, or characteristic, but every embodiment may not necessarilyinclude the particular feature, structure, or characteristic. Moreover,such phrases are not necessarily referring to the same embodiment.Further, when a particular feature, structure, or characteristic isdescribed in connection with an embodiment, that feature, structure, orcharacteristic may be used in connection with features, structures, orcharacteristics of other embodiments whether or not explicitlydescribed.

The term “about” as used herein includes the recited number ±10%. Thus,“about ten” means 9 to 11.

As used herein, “at %” means atomic percentage which is calculated basedon the number of atoms using the following formula:

Atomic % (at %)=100*((number of atoms of 1 component)/(number of atomsof all components).Atomic percentage can also be calculated based on the number of molesusing the formula:Atomic % (at %)=100*((number of moles of 1 component)/(number of molesof all components)).

As used herein, “electron percolation” means the transport of anelectron through a material. In cases wherein an electron percolatesthrough a single material, such as strontium iron cobalt molybdenumoxide, electron percolation means that there is a path for the electronthrough a layer using that material only. For example, if a compositematerial has a first material and a second material and electronspercolate through the first material, this means that electrons do nothave to pass through the second material when moving through thecomposite.

As used herein, “operating temperature” means the operating temperatureof the fuel cell during steady state operation. Preferably, theoperating temperature of a fuel cell is the optimal operatingtemperature that results in the most efficient fuel cell operation basedon the fuel cell's structure and materials used to form the fuel cell,i.e. the materials of the anode layer, electrolyte layer(s), cathodelayer, etc.

As used herein, “reduction” or “reducing” means the process of removingoxygen from a material, such as an anode layer, at a reductiontemperature and in the presence of a reducing atmosphere having a lowoxygen partial pressure, such as an H₂ atmosphere, H₂ and nitrogenatmosphere, or another inter gas atmosphere.

The basic operation of a solid oxide fuel cell is described in U.S. Pat.No. 9,525,179. Air flows into the system through an air inlet. As theair flows past the cathode layer, oxygen atoms are reduced within thecathode layer to create oxygen ions (O²⁻) which flow towards theelectrolyte layer. The oxygen ions travel through the electrolyte layerand into the anode layer, and then react with hydrogen gas at the anodelayer. The reaction between the oxygen ions and the hydrogen gas at theanode layer creates H₂O and electrons (e⁻). These electrons flow fromthe anode layer into the electronic circuit and back into the cathodelayer. The electronic circuit uses the flow of electrons to power adevice and the cathode layer uses the electrons to reduce oxygen atomsand start the process all over again. The chemical reactions for thefuel cell system can be expressed as follows:

-   -   Anode Reaction: 2H₂+2O²⁻→2H₂O+4e⁻    -   Cathode Reaction: O₂+4e⁻→2O²⁻    -   Overall Cell Reaction: 2H₂+O₂→2H₂O.

In some embodiments, the present invention provides an oxide compositionof formula (I):

SrFe_(x)Co_(((1−x)/2))Mo_(((1−x)/2))O_(3±δ)  (I)

wherein:

-   -   x is about 0.1-0.5; and    -   δ is about 0-1.5.

The ratios between the metals are measured as atomic percentage (at %).

In some embodiments, x is about 0.1-0.5, about 0.1-0.4, about 0.1-0.3,about 0.1-0.2, about 0.2-0.5, about 0.2-0.4, about 0.2-0.3, about0.3-0.5, about 0.3-0.4, or about 0.4-0.5. In some embodiments, x isabout 0.2. In some embodiments, x is about 0.1.

The variable δ in the above compositions represents an oxygen deficiencyand/or surplus in the composition. The value of δ is dependent ontemperature and the oxidation state of iron, cobalt, and molybdenum inthe composition. Additionally, the value of δ may vary depending on thepartial pressure of oxygen in the atmosphere and within the anodeitself. In some embodiments, δ is about 0-1.5, about 0-1, about 0-0.5,about 0.5-1.5, or about 1.0-1.5.

The measured atomic ratios for Sr, Fe, Co, Mo, and O may differ from thetheoretical ratios.

In some embodiments, the present invention provides a solid oxide fuelcell (SOFM) comprising:

-   -   (a) a cathode layer;    -   (b) an electrolyte layer; and    -   (c) an anode layer comprising a strontium iron cobalt molybdenum        (SFCM) oxide composition.

In some embodiments, the SOFC comprises a cathode layer. In someembodiments, the materials that can be used for the cathode layerinclude, but are not limited to, composite materials having (1) amaterial selected from the group consisting of lanthanum strontiumcobalt iron oxide (LSCF), barium strontium cobalt iron oxide (BSCF),samarium strontium cobalt iron oxide (SSCF), samarium strontium cobaltoxide (SSC), and lanthanum strontium manganate (LSM); and (2) a materialselected from the group consisting of: yttria stabilized zirconia (YSZ),scandia stabilized zirconia (SSZ), gadolinia doped ceria (GDC), samariadoped ceria (SDC), samaria-neodymium doped ceria (SNDC), erbiastabilized bismuth oxide (ESB), dysprosium tungsten stabilized bismuthoxide (DWSB), yttria stabilized bismuth oxide (YSB), and strontium andmagnesium doped lanthanum gallate (LSGM). In some embodiments, thematerial used for the cathode layer comprises SSC-GDC.

In some embodiments, the cathode layer may be composed of a singlematerial selected from the group consisting of lanthanum strontiumcobalt iron oxide (LSCF), barium strontium cobalt iron oxide (BSCF),samarium strontium cobalt iron oxide (SSCF), lanthanum strontiummanganate (LSM). In another embodiment, the cathode layer may compriseyttria stabilized zirconia (YSZ), scandia stabilized zirconia (SSZ),gadolinia doped ceria (GDC), samaria doped ceria (SDC),samaria-neodymium doped ceria (SNDC), erbia stabilized bismuth oxide(ESB), dysprosium tungsten stabilized bismuth oxide (DWSB), yttriastabilized bismuth oxide (YSB), and strontium and magnesium dopedlanthanum gallate (LSGM).

In some embodiments, the SOFC comprises an electrolyte layer. In someembodiments, the materials that can used for the electrolyte layerinclude, but are not limited to, yttria stabilized zirconia (YSZ),scandia stabilized zirconia (SSZ), gadolinia doped ceria (GDC), samariadoped ceria (SDC), samaria-neodymium doped ceria (SNDC), erbiastabilized bismuth oxide (ESB), yttria stabilized bismuth oxide (YSB),strontium and magnesium doped lanthanum gallate (LSGM), and combinationsthereof. The electrolyte layer in some embodiments may also includemultiple dopants and stabilizers. In some embodiments, the electrolytelayer comprises GDC.

In some embodiments, the SOFC comprises an anode layer. In someembodiments, the anode layer comprises an oxide composition. In someembodiments, the anode layer comprises various compositions of strontiumiron cobalt molybdenum oxide (SFCM). SFCM compositions have been foundto be compatible with intermediate- and low-temperature SOFCs andprovide high conductivity, reduction-oxidation stability, andcompatibility with hydrocarbon and sulfur-containing fuels. Furthermore,these materials avoid drawbacks associated with traditional Ni-basedoxide anode materials.

SFCM materials have high electronic conductivity when reduced at lowtemperatures. Being able to reduce the anode layer at low temperaturesreduces damage to other layers within the fuel cell that may besensitive to temperature. Such temperature sensitive layers may includethe electrolyte layer and/or the cathode layer. According to someembodiments, SFCM anode materials have high conductivity when reduced ata temperature that is similar to the operating temperature of the SOFC.If a material can be reduced at temperatures similar to the operatingtemperature of the SOFC, the anode layer can be reduced in situ, meaningthat a separate reducing operation during the fabrication of the SOFC isunnecessary. In some embodiments, the anode material has a highconductivity when reduced at a temperature of less than 850° C. In someembodiments, the anode material has a high conductivity when reduced ata temperature of less than 650° C. In some embodiments, the anodematerial is reduced in situ.

In some embodiments, the crystal structure of the anode layer isperovskite. In some embodiments, the anode layer includes only oxidematerials.

In some embodiments, the anode layer has a high conductivity attemperatures below 900° C., below 850° C., below 650° C., below 600° C.,below 450° C., or below 400° C. In some embodiments, the anode layer hasa high conductivity at temperatures between 350° C. and 900° C., 350° C.and 850° C., 350° C. and 650° C., 350° C. and 600° C., 350° C. and 450°C., 350° C. and 400° C., 400° C. and 900° C., 400° C. and 850° C., 400°C. and 650° C., 400° C. and 600° C., 400° C. and 450° C., 450° C. and900° C., 450° C. and 650° C., 450° C. and 600° C., 600° C. and 900° C.,600° C. and 850° C., 600° C. and 650° C., 650° C. and 900° C., 650° C.and 850° C., or 850° C. and 950° C. In some embodiments, the anode layerhas a high conductivity at temperatures below 650° C. In someembodiments, the anode layer has a high conductivity at temperaturesbelow 600° C.

In some embodiments, the anode layer has a conductivity of at least 10S/cm when measured at a temperature less than 850° C. In someembodiments, the anode layer has a conductivity of at least 10 S/cm whenmeasured at a temperature less than 650° C. In some embodiments, theanode layer has a conductivity between 10 S/cm and 100 S/cm, 10 S/cm and50 S/cm, 10 S/cm and 40 S/cm, 10 S/cm and 35 S/cm, 10 S/cm and 30 S/cm,30 S/cm and 100 S/cm, 30 s/cm and 50 S/cm, 30 S/cm and 40 S/cm, 30 S/cmand 35 S/cm, 35 S/cm and 100 S/cm, 35 S/cm and 50 S/cm, 35 S/cm and 40S/cm, 40 S/cm and 100 S/cm, 40 S/cm and 50 S/cm, or 50 S/cm and 100 S/cmwhen measured at a temperature less than 850° C. In some embodiments,the anode layer has a conductivity between 10 S/cm and 100 S/cm, 10 S/cmand 50 S/cm, 10 S/cm and 40 S/cm, 10 S/cm and 35 S/cm, 10 S/cm and 30S/cm, 30 S/cm and 100 S/cm, 30 s/cm and 50 S/cm, 30 S/cm and 40 S/cm, 30S/cm and 35 S/cm, 35 S/cm and 100 S/cm, 35 S/cm and 50 S/cm, 35 S/cm and40 S/cm, 40 S/cm and 100 S/cm, 40 S/cm and 50 S/cm, or 50 S/cm and 100S/cm when measured at a temperature less than 650° C.

In some embodiments, the anode layer has a conductivity between 10 S/cmand 100 S/cm, 10 S/cm and 50 S/cm, 10 S/cm and 40 S/cm, 10 S/cm and 35S/cm, 10 S/cm and 30 S/cm, 30 S/cm and 100 S/cm, 30 s/cm and 50 S/cm, 30S/cm and 40 S/cm, 30 S/cm and 35 S/cm, 35 S/cm and 100 S/cm, 35 S/cm and50 S/cm, 35 S/cm and 40 S/cm, 40 S/cm and 100 S/cm, 40 S/cm and 50 S/cm,or 50 S/cm and 100 S/cm when measured at a temperature of 850° C. Insome embodiments, the anode layer has a conductivity between 10 S/cm and100 S/cm, 10 S/cm and 50 S/cm, 10 S/cm and 40 S/cm, 10 S/cm and 35 S/cm,10 S/cm and 30 S/cm, 30 S/cm and 100 S/cm, 30 s/cm and 50 S/cm, 30 S/cmand 40 S/cm, 30 S/cm and 35 S/cm, 35 S/cm and 100 S/cm, 35 S/cm and 50S/cm, 35 S/cm and 40 S/cm, 40 S/cm and 100 S/cm, 40 S/cm and 50 S/cm, or50 S/cm and 100 S/cm when measured at a temperature of 650° C. In someembodiments, the anode layer has a conductivity between 10 S/cm and 100S/cm, 10 S/cm and 50 S/cm, 10 S/cm and 40 S/cm, 10 S/cm and 35 S/cm, 10S/cm and 30 S/cm, 30 S/cm and 100 S/cm, 30 s/cm and 50 S/cm, 30 S/cm and40 S/cm, 30 S/cm and 35 S/cm, 35 S/cm and 100 S/cm, 35 S/cm and 50 S/cm,35 S/cm and 40 S/cm, 40 S/cm and 100 S/cm, 40 S/cm and 50 S/cm, or 50S/cm and 100 S/cm when measured at a temperature of 500° C.

In some embodiments, the anode layer comprises a SFCM of Formula 1. Insome embodiments, the anode layer comprises a SFCM selected from thegroup consisting of SrFe_(0.1)Co_(0.45)Mo_(0.45)O₃,SrFe_(0.2)Co_(0.4)Mo_(0.4)O₃, SrFe_(0.34)Co_(0.33)Mo_(0.33)O₃, andSrFe_(0.5)Co_(0.25)Mo_(0.25)O₃. In some embodiments, the anode layercomprises SrFe_(0.2)Co_(0.4)Mo_(0.4)O₃. In some embodiments, the anodelayer comprises SrFe_(0.1)Co_(0.45)Mo_(0.45)O₃.

FIGS. 2A and 2B show exemplary fuel cells according to the invention. Asshown in FIG. 2A, in some embodiments, a fuel cell comprises a cathodelayer, an electrolyte bilayer, and an anode. As shown in FIG. 2B, insome embodiments, a fuel cell comprises a cathode layer, a cathodefunctional layer, an electrolyte layer and an anode layer.

In some embodiments, the SOFC comprises a cathode functional layer. Insome embodiments, the cathode functional layer improves the performanceof the cathode layer. In some embodiments, the material that can be usedfor cathode functional layer disposed over the electrolyte layerinclude, but are not limited to, La_(0.65)Sr_(0.5)Co₂O₅ (LSM),La_(0.6)Sr_(0.4)Co_(0.2)Fe_(0.8)O_(3-δ),La_(0.6)Sr_(0.4)Co_(0.2)Fe_(0.8)O_(3-δ) (LSCF),La_(0.8)Sr_(0.2)Cu_(0.9)Fe_(0.1)O_(2.5) (LSCuF), La_(0.7)Sr_(0.3)CoO₃(LSC), Sm_(0.5)Sr_(0.5)CoO₃ (SSC), SmBa_(0.5)Sr_(0.5)Co₂O₅ (SBSC),GdSrCo₂O₅ (GSC), LaBaCo₂O₅ (LBC), YBaCo₂O₅ (YBC), Nd_(1.8)Ce_(0.2)CuO₄(NCC), La_(0.8)Sr_(0.2)Co_(0.3)Mn_(0.1)Fe_(0.6)O₃ (LSCFM),La_(0.98)Ni_(0.6)Fe_(0.4)O₃ (LNF), La_(1.2)Sr_(0.8)NiO₄ (LSN),La_(0.7)Sr_(0.3)FeO₃ (LSF), La₂Ni_(0.6)Cu_(0.4)O₄ (LNC), silver, andtheir composites. The above compounds are listed in their stoichiometricratios, but as appreciated by one of ordinary skill in the art, theatomic ratios may vary slightly. Furthermore, while some of thesecompounds may require a high firing temperature, it is appreciated thatmodifiers may be used to lower the firing temperature of these materialsfor use in intermediate- and low-temperature solid-oxide fuel cells.

In some embodiments, the SOFC comprises an anode functional layer. Ananode functional layer is a separate anode layer with finer particlesizes to increase specific surface area, thereby increasing theelectrochemical reaction rate at the interface between anode layer andelectrolyte layer. In some embodiments, the anode functional layer isless porous than the rest of the anode layer. This may be achieved bycontrolling particle distribution and/or particle/solvent/binder ratios.In some embodiments, the anode functional layer is made of the samematerial as the anode layer itself. In some embodiments, the anode layeris made of a material that is different from the anode layer itself,such as Ni-GDC, Ni-perovskite, or with similar materials where Ni inreplaced with a different metal.

In some embodiments, the SOFC may also comprise structures for blockingthe diffusion of mobile dopant materials, e.g. iron, cobalt, ormolybdenum, out of SFCM, while maintaining the functionality of the SFCMas part of the SOFC. The diffusion of mobile dopant materials into anelectrolyte layer can decrease the conductivity of the electrolyte layerand reduce the efficiency of the SOFC. Iron, cobalt, or molybdenumdiffusions can also decrease the mechanical strength of the electrolytelayer and result in the formation of a phase or phases that cause highinterfacial resistance between the anode layer and the electrolyte.

Fabrication of Solid Oxide Fuel Cells Using a SFCM Anode

In some embodiments, the present invention provides a method of making asolid oxide fuel cell comprising a cathode layer, an electrolyte layer,and an anode layer, wherein the anode layer comprises a strontium ironcobalt molybdenum composition comprising:

-   -   (a) fabricating the cathode layer, the electrolyte layer, and        the anode layer; and    -   (b) forming a complete cell with the fabricated layers in (a).

In some embodiments, the temperature of any subsequent fabricationsteps, and the operating temperature of the solid oxide fuel cell, doesnot exceed 850° C. In some embodiments, the temperature of anysubsequent fabrication steps, and the operating temperature of the solidoxide fuel cell, does not exceed 650° C. In some embodimens, thetemperature of any subsequent steps, and the operating temperature ofthe solid oxide fuel cell, does not exceed 600° C.

In some embodiments, the present invention provides a method of making asolid oxide fuel cell comprising a cathode layer, a cathode functionallayer, an electrolyte layer, and an anode layer, wherein the anode layercomprises a strontium iron cobalt molybdenum composition comprising:

-   -   (a) fabricating the cathode layer, the cathode functional layer,        the electrolyte layer, and the anode layer; and    -   (b) forming a complete cell with the fabricated layers in (a).

In some embodiments, the temperature of any subsequent fabricationsteps, and the operating temperature of the solid oxide fuel cell, doesnot exceed 850° C. In some embodiments, the temperature of anysubsequent fabrication steps, and the operating temperature of the solidoxide fuel cell, does not exceed 650° C. In some embodimens, thetemperature of any subsequent steps, and the operating temperature ofthe solid oxide fuel cell, does not exceed 600° C.

In some embodiments, the electronic conducting SFCM anode material wascombined with pyrolyzable pore formers to facilitate adequate fueldiffusion through the ceramic anode after firing. A cross sectionalscanning electron microscope (SEM) image of a complete solid oxideelectrolyte fuel cell (SOFC) prepared with a SFCM anode material thatwas combined with pyrolyzable pore formers is shown in FIG. 7.

While the method of Example 1 describes fabricating four layers (anode,electrolyte, cathode functional layer, and cathode), it is appreciatedthat the completed fuel cell may include any number of additionallayers. For example, but not limited thereto, the completed fuel cellmay include a metallic contact layer and/or an electrolyte layer havingtwo layers (i.e. electrolyte bilayer).

In some embodiments, the SFCM is reduced before fabrication of the anodelayer. It is preferable that the reduction temperature for the anodelayer be keep as low as possible within the ranges described above,while still achieving sufficient oxygen removal and conductivity. Lowreduction temperature is preferred because other layers in the fuel cellmay be susceptible to temperature, thus resulting in, for example,atomic diffusion, annealing, and/or phase changes within or between theother layers. A high reducing temperature that alters thismicrostructure may be detrimental to the conductivity of the anode layerand the operating efficiency of the fuel cell. In some embodiments, theSFCM is not reduced before fabrication of the anode layer.

In some embodiments, the anode layer of the completed fuel cell is notreduced in in the completed fuel cell, but is reduced in situ instead.In other words, the anode layer is reduced during fuel cell operation.Since the anode layer is capable of being reduced at a temperature nohigher than the processing temperature, in situ reduction of the anodelayer is possible. In situ reduction of the anode layer of the completedfuel cell decreases processing costs.

In addition to reducing the anode layer, additional processing steps maybe performed on the completed fuel cell. In some embodiments, additionalprocessing steps are not performed at temperatures that exceed 850° C.In some embodiments, additional processing steps are not performed attemperatures that exceed 650° C. In some embodiments, additionalprocessing steps are not performed at temperatures that exceed 600° C.Additional processing temperatures may be performed at any appropriatetemperature, including temperatures as low as 0° C.

In some embodiments, the operating temperature of the SOFC does notexceed 850° C. In some embodiments, the operating temperature of theSOFC does not exceed 650° C. In some embodiments, the operatingtemperature of the SOFC is at least 350° C. to ensure efficientperformance of the SOFC. In some embodiments, the operating temperatureof the SOFC is between 350° C. and 850° C., 350° C. and 650° C., 350° C.and 550° C., 350° C. and 450° C., 450° C. and 850° C., 450° C. and 650°C., 450° C. and 550° C., 550° C. and 850° C., 550° C. and 650° C., or650° C. and 850° C. In some embodiments, the operating temperature ofthe SOFC is between 450° C. and 650° C.

Power density is the amount of power (time rate of energy transfer) perunit volume. In some embodiments, the power density of the SOFC is high.In some embodiments, the high peak power density of the SOFC is between300 mW/cm² and 800 mW/cm², 300 mW/cm² and 600 mW/cm², 300 mW/cm² and 500mW/cm², 500 mW/cm² and 800 mW/cm², 500 mW/cm² and 600 mW/cm², or 600mW/cm² and 800 mW/cm² when measured at 450° C. In some embodiments, thehigh peak power density of the SOFC is between 300 mW/cm² and 800mW/cm², 300 mW/cm² and 600 mW/cm², 300 mW/cm² and 500 mW/cm², 500 mW/cm²and 800 mW/cm², 500 mW/cm² and 600 mW/cm², or 600 mW/cm² and 800 mW/cm²when measured at 500° C. In some embodiments, the high peak powerdensity of the SOFC is between 300 mW/cm² and 800 mW/cm², 300 mW/cm² and600 mW/cm², 300 mW/cm² and 500 mW/cm², 500 mW/cm² and 800 mW/cm², 500mW/cm² and 600 mW/cm², or 600 mW/cm² and 800 mW/cm² when measured at650° C.

The foregoing description of the specific embodiments will so fullyreveal the general nature of the invention that others can, by applyingknowledge within the skill of the art, readily modify and/or adapt forvarious applications such specific embodiments, without undueexperimentation, without departing from the general concept of thepresent invention. Therefore, such adaptations and modifications areintended to be within the meaning and range of equivalents of thedisclosed embodiments, based on the teaching and guidance presentedherein. It is to be understood that the phraseology or terminologyherein is for the purpose of description and not of limitation, suchthat the terminology or phraseology of the present specification is tobe interpreted by the skilled artisan in light of the teachings andguidance.

EXAMPLES

The following examples are illustrative and non-limiting, of theproducts and methods described herein. Suitable modifications andadaptations of the variety of conditions, formulations, and otherparameters normally encountered in the field and which are obvious tothose skilled in the art in view of this disclosure are within thespirit and scope of the invention.

Example 1

Compositions of SrFe_(0.1)Co_(0.45)Mo_(0.45)O₃,SrFe_(0.2)Co_(0.4)Mo_(0.4)O₃, SrFe_(0.34)Co_(0.33)Mo_(0.33)O₃, andSrFe_(0.5)Co_(0.25)Mo_(0.25)O₃ having Co to Mo in the ratio of 1:1 weresynthesized using the glycine-nitrate combustion method modified usingcitric acid. Stoichiometric amounts of strontium nitrate (Alfa Aesar99.0%), iron nitrate nonahydrate (Sigma Aldrich 99.95%), cobalt nitratehexahydrate (Alfa Aesar 98%-102%) and ammonium molybdate (para)tetrahydrate (Alfa Aesar 99%) were dissolved in de-ionized waterseparately. Glycine (glycine to nitrate in the ratio of 1:1) wasdissolved in de-ionized water and subsequently, citric acid (with 20%glycine by weight) was added to maintain a pH of approximately 2. Thestrontium salt solutions were poured into the glycine-citrate mixtureand heated on a hot plate to evaporate solvent and to form a viscousgel. The temperature of the hot plate was increased to 350° C., whereinauto ignition occurred. At this higher temperature, the metal nitratesdecompose to metal oxides and oxides of nitrogen (see, e.g., Singh, K.,et al., Indian J. Eng. Mater. Sci. 13:525-530 (2006)).

The residues of the reaction were ground and calcined at 1100° C. for 4hours to obtain powders. The SFCM anode supported SOFCs were fabricatedby tape-casting technique. The tape casting technique is a well-knowncolloidal shaping technique for large-area, thin, flat ceramic sheets ormembranes (see, e.g., J.A. Lewis, J. Am. Chem. Soc. 83:2341-2359(2000)). The anode scaffold was prepared by mixingSrFe_(0.2)Co_(0.4)Mo_(0.4)O₃ (SFCM#3) and 2% cobalt doped GDC (in aweight ratio of 2:1). Poly(methyl methacrylate) (Soken Chemical &Engineering Co., Ltd, Tokyo, Japan), used as a pore former, was added toobtain an initial porosity of 40 vol %. Polyvinyl butyral, butyl benzylphthalate, and fish oil were used as binder, plasticizer, anddispersant, respectively. For SFCM tape-casting recipe, ethanol was usedas solvent. Prepared raw tapes (i.e. before firing) and 25-30 μm raw GDCelectrolyte tape were laminated together and co-fired at 1200° C. for 4hours.

The electrolyte surface of the half-cell was deposited with a 5-7 μmCo-doped GDC as cathode functional layer (CFL) initially. The CFL wasprepared by ball milling GDC powder and 2 mol % cobalt nitrates inethanol overnight. Subsequently, ethanol was evaporated and heat treatedat 400° C. for 1 hour. The mixed powder was made into a paste and brushpainted on the half-cell. The half-cell was dried in an oven at 70° C.for 1 hour. Subsequently, Sr_(0.5)Sm_(0.5)CoO_(3-δ)-GDC (SSC-GDC)cathode was applied and the assembly was co-fired at 950° C. for 2hours. Ag metal was used as the current collector at both electrodes.The schematic of the SFCM based anode supported cell is shown in FIG. 2.An optimized quantity of Ni-GDC (loading of approximately 10 wt %) wasinfiltrated into the anode. A 400° C. burnout process was performedduring each infiltration interval and a final heat treatment wasperformed at 800° C. for 1 hour.

Typically ceramic anode based SOFCs require high operating temperatureeither because the conductivity is too low at low temperatures or thecatalytic activity is not sufficient. As shown in FIG. 4,SrFe_(0.2)Co_(0.4)Mo_(0.4)O₃ (SFCM#3) and SrFe_(0.1)Co_(0.45)Mo_(0.45)O₃(SFCM#2) based anode-supported cell was shown to have high electronicconductivity (30 S/cm measured at 650° C.) and has shown highperformance at low temperatures—better than conventional Ni-GDC cermetsupported cells. A high peak Power Density (PD) of 460 mW/cm² at 500° C.and 300 mW/cm² at 450° C. with current density of 1.0 A/cm² and 0.6A/cm², respectively have been achieved with an SOFC having an anodelayer comprising SrFe_(0.2)Co_(0.4)Mo_(0.4)O₃as shown in FIG. 5.

Shown in FIG. 6 are Nyquist plots of the electrochemical impedancemeasurements of an SOFC having an anode layer comprisingSrFe_(0.2)Co_(0.4)Mo_(0.4)O₃. A CFL was incorporated at the interface ofelectrolyte and cathode to improve the cathode performance.SrFe_(0.2)Co_(0.4)Mo_(0.4)O₃ by itself is not a catalytically activematerial for hydrogen oxidation at low temperatures. Thus, Ni-GDC wasinfiltrated into the SFCM scaffold and the low temperature heattreatment process retained the nanomorphology. The SEM micrographs ofthe post-tested SrFe_(0.2)Co_(0.4)Mo_(0.4)O₃ anode support cell areshown in FIGS. 7-10. Shown in FIG. 7 is the cross-sectional SEM imageshowing the porous SFCM/GDC electrolyte/CFL/cathode. Shown in FIGS. 8-10are cross-sectional SEM images showing the SFCM microstructure withNi-GDC nano-particles deposited on the surface.

Having now fully described this invention, it will be understood bythose of ordinary skill in the art that the same can be performed withina wide and equivalent range of conditions, formulations and otherparameters without affecting the scope of the invention or anyembodiment thereof. All patents, patent applications, and publicationscited herein are fully incorporated by reference herein in theirentirety.

1.-28. (canceled)
 29. An oxide composition comprising:SrM¹ _(x)M² _(((1−x)/2))Mo_(((1−x)/2))O_(3±δ) wherein: M¹ is atransition metal; M² is a transition metal; wherein M¹ does not equalM², and neither M¹ nor M² is Mo; x is about 0.1-0.5; and δ is about0-1.5.
 30. An oxide composition comprising:SrM¹ _(x)M² _(y)Mo_(z)O₃ wherein: M¹ is a transition metal; M² is atransition metal; wherein M¹ does not equal M², and neither M¹ nor M² isMo; x is about 0.1-0.5; y is about 1−x; and z is about 1−x. 31.-46.(canceled)
 47. The oxide composition of claim 29, wherein x is about0.1-0.4.
 48. The oxide composition of claim 30, wherein x is about0.1-0.4.
 49. The oxide composition of claim 29, wherein x is about0.1-0.3.
 50. The oxide composition of claim 30, wherein x is about0.1-0.3.
 51. The oxide composition of claim 29, wherein x is about0.1-0.25.
 52. The oxide composition of claim 30, wherein x is about0.1-0.25.
 53. The oxide composition of claim 29, wherein M¹ is Fe and M²is Co.
 54. The oxide composition of claim 30, wherein M¹ is Fe and M² isCo.
 55. The oxide composition of claim 29, comprisingSrFe_(0.1)Co_(0.45)Mo_(0.45)O₃, SrFe_(0.2)Co_(0.4)Mo_(0.4)O₃,SrFe_(0.34)Co_(0.33)Mo_(0.33)O₃, or SrFe_(0.5)Co_(0.25)Mo_(0.25)O₃. 56.The oxide composition of claim 30, comprisingSrFe_(0.1)Co_(0.45)Mo_(0.45)O₃, SrFe_(0.2)Co_(0.4)Mo_(0.4)O₃,SrFe_(0.34)Co_(0.33)Mo_(0.33)O₃, or SrFe_(0.5)Co_(0.25)Mo_(0.25)O₃. 57.The oxide composition of claim 29, which comprisesSrFe_(0.2)Co_(0.4)Mo_(0.4)O₃.
 58. The oxide composition of claim 30,which comprises SrFe_(0.2)Co_(0.4)Mo_(0.4)O₃.
 59. The oxide compositionof claim 29, which comprises SrFe_(0.1)Co_(0.45)Mo_(0.45)O₃.
 60. Theoxide composition of claim 30, which comprisesSrFe_(0.1)Co_(0.45)Mo_(0.45)O₃.
 61. The oxide composition of claim 29,wherein the oxide composition has a conductivity of between 10 S/cm and100 S/cm when measured at a temperature between 350° C. and 850° C. 62.The oxide composition of claim 29, wherein the oxide composition isinfiltrated with a multivalent transition metal.
 63. The oxidecomposition of claim 62, wherein the multivalent transition metal is Nior Ni-GDC.
 64. The oxide composition of claim 29, wherein the oxidecomposition is porous.